Package | Description |
---|---|
org.orekit.files.ccsds.ndm.odm.omm |
This package contains class managing CCSDS Orbit Mean-Elements Message.
|
org.orekit.propagation.analytical.tle |
This package provides classes to read and extrapolate tle's.
|
org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
Modifier and Type | Method and Description |
---|---|
TLE |
Omm.generateTLE()
Generate TLE from OMM file.
|
Modifier and Type | Field and Description |
---|---|
protected TLE |
TLEPropagator.tle
Initial state.
|
Modifier and Type | Method and Description |
---|---|
TLE |
TLEPropagator.getTLE()
Get the underlying TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE)
Convert Spacecraft State into TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE,
TimeScale utc,
Frame teme)
Convert Spacecraft State into TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE,
TimeScale utc,
Frame teme,
double epsilon,
int maxIterations)
Convert Spacecraft State into TLE.
|
TLE |
FieldTLE.toTLE()
Convert FieldTLE into TLE.
|
Modifier and Type | Method and Description |
---|---|
static TLEPropagator |
TLEPropagator.selectExtrapolator(TLE tle)
Selects the extrapolator to use with the selected TLE.
|
static TLEPropagator |
TLEPropagator.selectExtrapolator(TLE tle,
AttitudeProvider attitudeProvider,
double mass)
Selects the extrapolator to use with the selected TLE.
|
static TLEPropagator |
TLEPropagator.selectExtrapolator(TLE tle,
AttitudeProvider attitudeProvider,
double mass,
Frame teme)
Selects the extrapolator to use with the selected TLE.
|
static TLEPropagator |
TLEPropagator.selectExtrapolator(TLE tle,
Frames frames)
Selects the extrapolator to use with the selected TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE)
Convert Spacecraft State into TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE,
TimeScale utc,
Frame teme)
Convert Spacecraft State into TLE.
|
static TLE |
TLE.stateToTLE(SpacecraftState state,
TLE templateTLE,
TimeScale utc,
Frame teme,
double epsilon,
int maxIterations)
Convert Spacecraft State into TLE.
|
Constructor and Description |
---|
DeepSDP4(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass)
Constructor for a unique initial TLE.
|
DeepSDP4(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass,
Frame teme)
Constructor for a unique initial TLE.
|
SGP4(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass)
Constructor for a unique initial TLE.
|
SGP4(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass,
Frame teme)
Constructor for a unique initial TLE.
|
TLEPropagator(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass)
Protected constructor for derived classes.
|
TLEPropagator(TLE initialTLE,
AttitudeProvider attitudeProvider,
double mass,
Frame teme)
Protected constructor for derived classes.
|
Modifier and Type | Method and Description |
---|---|
TLE |
TLEPropagatorBuilder.getTemplateTLE()
Getter for the template TLE.
|
Constructor and Description |
---|
TLEPropagatorBuilder(TLE templateTLE,
PositionAngle positionAngle,
double positionScale)
Build a new instance.
|
TLEPropagatorBuilder(TLE templateTLE,
PositionAngle positionAngle,
double positionScale,
DataContext dataContext)
Build a new instance.
|
TLEPropagatorBuilder(TLE templateTLE,
PositionAngle positionAngle,
double positionScale,
DataContext dataContext,
double epsilon,
int maxIterations)
Build a new instance.
|
TLEPropagatorBuilder(TLE templateTLE,
PositionAngle positionAngle,
double positionScale,
double epsilon,
int maxIterations)
Build a new instance.
|
Copyright © 2002-2022 CS GROUP. All rights reserved.